View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 57935U 26145.40596227 +.00000000 +00000-0 +47137-4 0 00001
2 57935 53.1620 27.5564 0001140 80.9018 279.2114 15.34396768 07
| Epoch (UTC): | 25 May 2026 09:44:35 |
| Eccentricity: | 0.0001140 |
| inclination: | 53.1620° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 27.5564° |
| argument of perigee: | 80.9018° |
| revolutions per day: | 15.34396768 |
| mean anomaly at epoch: | 279.2114° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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